kodning som gjordes hos bragde

EENX15_LQR/Arduino_skal.h

@@ -0,0 +1,228 @@
+//
+// Academic License - for use in teaching, academic research, and meeting
+// course requirements at degree granting institutions only.  Not for
+// government, commercial, or other organizational use.
+//
+// File: Arduino_skal.h
+//
+// Code generated for Simulink model 'Arduino_skal'.
+//
+// Model version                  : 1.1
+// Simulink Coder version         : 9.5 (R2021a) 14-Nov-2020
+// C/C++ source code generated on : Thu Apr 15 22:06:00 2021
+//
+// Target selection: ert.tlc
+// Embedded hardware selection: AMD->x86-64 (Windows64)
+// Code generation objectives:
+//    1. Execution efficiency
+//    2. RAM efficiency
+// Validation result: Not run
+//
+#ifndef RTW_HEADER_Arduino_skal_h_
+#define RTW_HEADER_Arduino_skal_h_
+//#include <cstring>
+#include "rtwtypes.h"
+//#include "rtw_continuous.h"
+//#include "rtw_solver.h"
+
+// Model Code Variants
+
+// Macros for accessing real-time model data structure
+#ifndef rtmGetErrorStatus
+#define rtmGetErrorStatus(rtm)         ((rtm)->errorStatus)
+#endif
+
+#ifndef rtmSetErrorStatus
+#define rtmSetErrorStatus(rtm, val)    ((rtm)->errorStatus = (val))
+#endif
+
+#ifndef rtmGetStopRequested
+#define rtmGetStopRequested(rtm)       ((rtm)->Timing.stopRequestedFlag)
+#endif
+
+#ifndef rtmSetStopRequested
+#define rtmSetStopRequested(rtm, val)  ((rtm)->Timing.stopRequestedFlag = (val))
+#endif
+
+#ifndef rtmGetStopRequestedPtr
+#define rtmGetStopRequestedPtr(rtm)    (&((rtm)->Timing.stopRequestedFlag))
+#endif
+
+#ifndef rtmGetT
+#define rtmGetT(rtm)                   (rtmGetTPtr((rtm))[0])
+#endif
+
+#ifndef rtmGetTPtr
+#define rtmGetTPtr(rtm)                ((rtm)->Timing.t)
+#endif
+
+#ifndef ODE3_INTG
+#define ODE3_INTG
+
+// ODE3 Integration Data
+struct ODE3_IntgData {
+  real_T *y;                           // output
+  real_T *f[3];                        // derivatives
+};
+
+#endif
+
+// Class declaration for model Arduino_skal
+class Arduino_skalModelClass {
+  // public data and function members
+ public:
+  // Block signals and states (default storage) for system '<Root>'
+  struct DW {
+    real_T Sum4[4];                    // '<Root>/Sum4'
+  };
+
+  // Continuous states (default storage)
+  struct X {
+    real_T Integrator1_CSTATE[4];      // '<Root>/Integrator1'
+  };
+
+  // State derivatives (default storage)
+  struct XDot {
+    real_T Integrator1_CSTATE[4];      // '<Root>/Integrator1'
+  };
+
+  // State disabled
+  struct XDis {
+    boolean_T Integrator1_CSTATE[4];   // '<Root>/Integrator1'
+  };
+
+  // Constant parameters (default storage)
+  struct ConstP {
+    // Expression: [100;200]
+    //  Referenced by: '<Root>/vartejag'
+
+    real_T vartejag_Value[2];
+
+    // Expression: A
+    //  Referenced by: '<Root>/Gain4'
+
+    real_T Gain4_Gain[16];
+
+    // Expression: C
+    //  Referenced by: '<Root>/Gain6'
+
+    real_T Gain6_Gain[8];
+
+    // Expression: L
+    //  Referenced by: '<Root>/Gain2'
+
+    real_T Gain2_Gain[8];
+
+    // Expression: B
+    //  Referenced by: '<Root>/Gain3'
+
+    real_T Gain3_Gain[4];
+  };
+
+  // Real-time Model Data Structure
+  struct RT_MODEL {
+    const char_T *errorStatus;
+    //RTWSolverInfo solverInfo;
+    X *contStates;
+    int_T *periodicContStateIndices;
+    real_T *periodicContStateRanges;
+    real_T *derivs;
+    boolean_T *contStateDisabled;
+    boolean_T zCCacheNeedsReset;
+    boolean_T derivCacheNeedsReset;
+    boolean_T CTOutputIncnstWithState;
+    real_T odeY[4];
+    real_T odeF[3][4];
+    ODE3_IntgData intgData;
+
+    //
+    //  Sizes:
+    //  The following substructure contains sizes information
+    //  for many of the model attributes such as inputs, outputs,
+    //  dwork, sample times, etc.
+
+    struct {
+      int_T numContStates;
+      int_T numPeriodicContStates;
+      int_T numSampTimes;
+    } Sizes;
+
+    //
+    //  Timing:
+    //  The following substructure contains information regarding
+    //  the timing information for the model.
+
+    struct {
+      uint32_T clockTick0;
+      time_T stepSize0;
+      uint32_T clockTick1;
+      SimTimeStep simTimeStep;
+      boolean_T stopRequestedFlag;
+      time_T *t;
+      time_T tArray[2];
+    } Timing;
+  };
+
+  // model initialize function
+  void initialize();
+
+  // model step function
+  void step();
+
+  // Constructor
+  Arduino_skalModelClass();
+
+  // Destructor
+  ~Arduino_skalModelClass();
+
+  // Real-Time Model get method
+  Arduino_skalModelClass::RT_MODEL * getRTM();
+
+  // private data and function members
+ private:
+  // Block signals and states
+  DW rtDW;
+  X rtX;                               // Block continuous states
+
+  // Real-Time Model
+  RT_MODEL rtM;
+
+  // Continuous states update member function
+  //void rt_ertODEUpdateContinuousStates(RTWSolverInfo *si );
+
+  // Derivatives member function
+  void Arduino_skal_derivatives();
+};
+
+// Constant parameters (default storage)
+extern const Arduino_skalModelClass::ConstP rtConstP;
+
+//-
+//  These blocks were eliminated from the model due to optimizations:
+//
+//  Block '<Root>/Kr' : Eliminated nontunable gain of 1
+
+
+//-
+//  The generated code includes comments that allow you to trace directly
+//  back to the appropriate location in the model.  The basic format
+//  is <system>/block_name, where system is the system number (uniquely
+//  assigned by Simulink) and block_name is the name of the block.
+//
+//  Use the MATLAB hilite_system command to trace the generated code back
+//  to the model.  For example,
+//
+//  hilite_system('<S3>')    - opens system 3
+//  hilite_system('<S3>/Kp') - opens and selects block Kp which resides in S3
+//
+//  Here is the system hierarchy for this model
+//
+//  '<Root>' : 'Arduino_skal'
+
+#endif                                 // RTW_HEADER_Arduino_skal_h_
+
+//
+// File trailer for generated code.
+//
+// [EOF]
+//

EENX15_LQR/EENX15_LQR.ino

@@ -23,7 +23,10 @@ float motorAngularSpeed = 0;
 
 /** PWM signal applied to the motor's driver 255 is 100% */
 int speed;
+int Va;
 int safe_angle;
+float force;
+int PWM;
 
 
 //gyro stuff
@@ -160,7 +163,6 @@ void set_test_speed(){
   analogWrite(MotorSpeedA, speed); //First experiment wheel
   Serial.print("Rads per second: "); Serial.println(rps); //ca. 56 tick per rotation, 6.26 rads per rotation
   Serial.print("Speed: "); Serial.println(speed); //ca. 56 tick per rotation, 6.26 rads per rotation
-
   temp_counter += 3;
 }
 */
@@ -172,31 +174,27 @@ void setSpeed(){
     float angle_r = angle_pitch_output * 0.318;
     float angle_speed_rs = rps;
     //speed = lqr_fullstate(position_m, speed_ms, angle_r, angle_speed_rs);/// 0.019608; // (0.20*255)
-    speed = lqr_fullstate(0, 0, angle_r, 0);/// 0.019608; // (0.20*255)
+    force = lqr_fullstate(0, 0, angle_r, 0);/// 0.019608; // (0.20*255)
     //speed = -22 * inputToControlSystem(0, 1);
-    if(speed<0){
+    if(force<0){
       digitalWrite(MotorPinB, CW);
       digitalWrite(MotorPinA, CCW);
     }
-    else if(speed>0){
+    else if(force>0){
       digitalWrite(MotorPinB, CCW);
       digitalWrite(MotorPinA, CW);
     }
     else {
-      speed = 0;
+      force = 0;
     }
-    if(speed!=0){ speed = constrain(speed, -255, 255);speed = calc_speed(speed); }
-    speed = abs(speed);
-    speed = constrain(speed, 0, 255);
-    analogWrite(MotorSpeedB, speed); //Wheel close to connections
-    analogWrite(MotorSpeedA, speed); //First experiment wheel
+    if(force!=0){Va = calc_speed(force, angle_speed_rs); }
+    Va = abs(Va);
+    PWM = 255*Va/12;
+    PWM = constrain(PWM, 0, 255);
+    analogWrite(MotorSpeedB, PWM); //Wheel close to connections
+    analogWrite(MotorSpeedA, PWM); //First experiment wheel
   } 
-  else{
-    speed = 0;
-    analogWrite(MotorSpeedB, speed);
-    analogWrite(MotorSpeedA, speed);
-  } 
-  Serial.print("Speed to motors: "); Serial.println(speed);
+  Serial.print("PWM to motors: "); Serial.println(PWM);
 }
 int directionA(){
   if(digitalRead(encoderA2) ==  HIGH){                             

EENX15_LQR/LQR.ino

@@ -138,7 +138,6 @@ void Arduino_skal_derivatives()
   _rtXdot->Integrator1_CSTATE[2] = Sum4[2];
   _rtXdot->Integrator1_CSTATE[3] = Sum4[3];
   
-  
   Integrator1_CSTATE[0] = Sum4[0] * (fastTimer/1000.0);
   Integrator1_CSTATE[1] = Sum4[1] * (fastTimer/1000.0);
   Integrator1_CSTATE[2] = Sum4[2] * (fastTimer/1000.0);

EENX15_LQR/lqr_fullstate.ino

@@ -26,13 +26,15 @@ float lqr_fullstate(float position_m, float speed_ms, float angle_r, float angle
   Serial.print("K calculation (force): "); Serial.println(result); 
   return result;
 }
-float calc_speed(float input) {
+float calc_speed(float input, float angle_speed_rs) {
   /*
   float a = -2971;
   float b = -0.9929;
   float c = 90.75;
   float radps = a * pow(speed, b) + c; ////// the response graph
   */
+
+  /*
   float scale = 1.5;
   input = abs(input)*0.30796; // scale down to rad/s (78,53/255)
   Serial.print("input: "); Serial.println(input); 
@@ -40,5 +42,16 @@ float calc_speed(float input) {
   result *= scale;
   Serial.print("calcspeed: "); Serial.println(result); 
   return result;
+  */
+  float I = (1/3)*1.74;
+  float km = 0.91*0.01;
+  float ke = 8.68*0.001*2*PI/60;
+  float Ir = I;
+  float Omega= angle_speed_rs;
+  
+  float result = (km*ke/(Ir*5-km))*Omega;
+  Serial.print("RESULT");
+  Serial.print(result);
+  return result;
   
 }